US8125215B2ActiveUtilityA1

Measuring vibrations of a turbo-machine rotor blade with the help of an induction sensor in high temperature

Assignee: ROKICKI EDWARDPriority: Jun 9, 2008Filed: Jun 3, 2009Granted: Feb 28, 2012
Est. expiryJun 9, 2028(~1.9 yrs left)· nominal 20-yr term from priority
G01H 1/006
54
PatentIndex Score
4
Cited by
4
References
4
Claims

Abstract

A method is disclosed of measuring vibrations on turbo-machine rotary turbine blades utilizing an induction sensor at high temperatures. A set of magnets produces a magnetic field which results in a measurement signal generated in the sensor's coil which then can be interpreted to measure the vibrations.

Claims

exact text as granted — not AI-modified
What is claimed is: 
     
       1. A method of measuring vibrations of turbo-machine rotary turbin blades using an induction sensor in a high temperature environment, the method comprising:
 placing the induction sensor which comprises a coil winding around a set of magnets in an engine housing such that a face of the induction sensor is positioned in the turbo-machine rotary turbine blade's rotation plane; 
 producing a magnetic field in front of the sensor's face through the set of magnets; 
 generating a measurement signal through the sensor's coil winding as a result of the turbo-machine rotary turbine blade's movement in the magnetic field; 
 amplifying the signal and sending such signal to a computer; and 
 wherein a substantially stable and substantially repeatable magnetic field is created in front of the sensor's face through the set of magnets, the magnets having different magnetic fields and different Curie temperatures, the Curie temperatures of the set of magnets being higher than the high temperature environment and the different between the Curie temperatures of at least two of the magnets being sufficiently different to effect a magnetic field sufficiently stable to induce eddy currents in the turbine blades. 
 
     
     
       2. The method of  claim 1  wherein the face of the induction sensor is separated from the turbo-machine rotary turbine's blade's working environment and from the engine housing by a ceramic screen. 
     
     
       3. The method of  claim 2  wherein a temperature gradient is created by the ceramic screen between the inside of the engine and the elements taken advantage of. 
     
     
       4. The method of  claim 1  wherein the set of magnets includes first and second magnets, with the first magnet having a higher Curie temperature than the second magnet, and the first magnet having an end that comprises the face of the sensor.

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